Linearized variable-dispersion spectrometers and related assemblies

ABSTRACT

Wavenumber linear spectrometers are provided including an input configured to receive electromagnetic radiation from an external source; collimating optics configured to collimate the received electromagnetic radiation; a dispersive assembly including first and second diffractive gratings, wherein the first diffraction grating is configured in a first dispersive stage to receive the collimated electromagnetic radiation and wherein the dispersive assembly includes at least two dispersive stages configured to disperse the collimated input; and an imaging lens assembly configured to image the electromagnetic radiation dispersed by the at least two dispersive stages onto a linear detection array such that the variation in frequency spacing along the linear detection array is no greater than about 10%.

CLAIM OF PRIORITY

The present application is a continuation of U.S. patent applicationSer. No. 13/428,247, filed Mar. 23, 2012 (now U.S. Pat. No. 8,797,530),which claims priority from U.S. Provisional Application No. 61/466,611,filed Mar. 23, 2011, the disclosures of which are hereby incorporatedherein by reference as if set forth in their entirety.

STATEMENT OF GOVERNMENT SUPPORT

This invention was made with government support under grant number2R44EY018021 awarded by National Institute of Health, National EyeInstitute. The United States Government has certain rights in thisinvention.

FIELD

The present inventive concept generally relates to imaging and, moreparticularly, to Fourier domain optical coherence tomography (FDOCT) andrelated systems and methods.

BACKGROUND

Dispersive optical elements disperse light by deviating the path oflight passing through them by an amount that varies with wavelength.Prisms and gratings are two types of dispersive optical elements. Inparticular, prisms disperse light because their geometry causes light ofdifferent wavelengths passing through them to be separated and deviatedby different amounts. In diffraction gratings, light passing through thegrating is diffracted into a series of orders caused by the interferenceof wavefronts emitted from each slit in the grating.

Dispersive optical elements are used in spectrometers. Spectrometers areused in fields including medicine, material sciences, chemistry,environmental sciences, and so on. Spectrometers use diffractive andrefractive dispersive optical elements including gratings and/or prismsto facilitate analyzing the spectral composition of sampled light.

As illustrated in FIG. 1, a conventional spectrometer 110 includes alight input entrance element 112 (Detector arm fiber) for receivinglight from an external source. More generally the light entrance element112 may be referred to as an electromagnetic radiation entrance. Thelight is passed through a first set of collimating optics 114(collimating lens) to a diffraction grating 116. The diffraction grating116 separates the light into various spectra. The separated light passesthrough a second set of focusing optics 118 to a detection element 120(detector).

Fourier-domain optical coherence tomography (FDOCT) uses a Fouriertransform of spectrum to calculate distribution of scatterers in asample. Digital Fourier transform algorithms typically rely on data thatis evenly spaced in frequency. However, gratings (for example,diffraction grating 116) disperse spectrum proportional to wavelength,not frequency. Thus, as illustrated in FIG. 2A, even spaced frequenciesdo not have even spacing on the detector 220 in a conventionalspectrometer 210. Thus, as illustrated in the graph of FIG. 2B,conventional spectrometers 210 may experience about a 50% change indispersion across a full spectrum.

U.S. Patent Application Publication No. 2009/0040521 entitled EVENFREQUENCY SPACING SPECTROMETER AND OPTICAL COHERENCE TOMOGRAPHY DEVICEto Hu et al. addresses this relatively high change in dispersion by aprism air-spaced with respect to a grating. This is also discussed inFOURIER DOMAIN OPTICAL COHERENCE TOMOGRAPHY WITH A LINEAR-IN-WAVENUMBERSPECTROMETER by Hu et al. Hu discusses using first and second dispersiveelements, for example, a grating and a prism, separated by an air gap toapproximately linearize the dispersion angle as a function ofwavenumber.

However, improved systems for reducing the overall change in dispersionmay be desired.

SUMMARY

Some embodiments of the present inventive concept provide wavenumberlinear spectrometers including an input configured to receiveelectromagnetic radiation from an external source; collimating opticsconfigured to collimate the received electromagnetic radiation; adispersive assembly including first and second diffractive gratings,wherein the first diffraction grating is configured in a firstdispersive stage to receive the collimated electromagnetic radiation andwherein the dispersive assembly includes at least two dispersive stagesconfigured to disperse the collimated input; and an imaging lensassembly configured to image the electromagnetic radiation dispersed bythe at least two dispersive stages onto a linear detection array suchthat the variation in frequency spacing along the linear detection arrayis no greater than about 10%.

In further embodiments, the dispersive assembly may include a prism. Thevariation in frequency spacing along the detection array may be nogreater than 5.0%.

In still further embodiments, the imaging lens assembly may beconfigured to image with pincushion distortion. The imaging lensassembly may further include pincushion distortion correction; thepresence of the pincushion distortion correction may further reduce thevariation in frequency spacing along the detection array to no greaterthan about 1.0%. The pincushion distortion correction may include awavefront modifier element positioned after a lens set that images withpincushion distortion and before a detector array. In certainembodiments, the wavefront modifier element may be an asphere.

In some embodiments, the dispersive assembly may be configured to beinterchangeable.

In further embodiments, a wavenumber span ranges from about 250 cm⁻¹ toabout 5100 cm⁻¹.

Still further embodiments provide wavenumber linear spectrometersincluding an input configured to receive electromagnetic radiation froman external source; collimating optics configured to collimate thereceived electromagnetic radiation; a dispersive assembly includingfirst and second dispersive elements, wherein the first dispersiveelement is a diffraction grating configured to receive the collimatedelectromagnetic radiation and wherein the second dispersive element is arefractive prism; and an imaging lens assembly including pincushiondistortion correction, wherein the imaging lens assembly is configuredto image the collimated electromagnetic radiation dispersed by thedispersive assembly onto a linear detection array, such that thevariation in frequency spacing along the linear detection array is nogreater than about 5.0%.

In some embodiments, the distortion correction is an asphere positionedafter a lens set in the imaging lens system, the presence of thedistortion correction further reducing the variation in frequencyspacing along the detection array to no greater than about 1.0%.

In further embodiments, the dispersive assembly may be configured to beinterchangeable.

In still further embodiments, a wavenumber span may range from about1000 cm⁻¹ to about 3000 cm⁻¹.

Some embodiments of the present inventive concept provide spectrometerassemblies including a dispersive assembly including first and seconddispersive stages, the first dispersive stage configured to receive acollimated input of electromagnetic radiation; and a lens assembly. Thefirst and second dispersive stages and the lens assembly combine toimage the collimated input of electromagnetic radiation dispersed onto alinear detection array, such that the variation in frequency spacingalong the detection array is less than about 10%. The dispersiveassembly is configured to be interchangeable.

Further embodiments of the present inventive concept provide Fourierdomain optical coherence tomography detection systems including awavenumber linear spectrometer, the wavenumber linear spectrometerincluding two diffractive gratings.

Still further embodiments of the present inventive concept provideFourier domain optical coherence tomography detection systems includingwavenumber linear spectrometer. The wavenumber linear spectrometerincluding a diffraction grating; a prism; and a lens assembly, the lensassembly comprising pincushion distortion correction.

BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings, which are included to provide a furtherunderstanding of the inventive concept and are incorporated in andconstitute a part of this application, illustrate certain embodiment(s)of the inventive concept. In the drawings:

FIG. 1 is a diagram illustrating a conventional spectrometer.

FIG. 2A is a diagram illustrating a conventional spectrometer havinguneven spacing at the detector of the spectrometer.

FIG. 2B is a graph illustrating a change in dispersion for thespectrometer illustrated in FIG. 2A.

FIG. 3A is a diagram illustrating a spectrometer including a dualgrating dispersive assembly in accordance with some embodiments of thepresent inventive concept.

FIG. 3B is a graph illustrating a change in dispersion for thespectrometer illustrated in FIG. 3A.

FIG. 4A is a diagram illustrating a spectrometer including a grismdispersive assembly in accordance with some embodiments of the presentinventive concept.

FIG. 4B is a graph illustrating a change in dispersion for thespectrometer illustrated in FIG. 4A.

FIGS. 5A and 5B are diagrams illustrating using barrel distortion tocompensate for pincushion distoration in accordance with someembodiments of the present inventive concept.

FIG. 6A is a block diagram illustrating a spectrometer including adistortion element in addition to a dispersive assembly in accordancewith some embodiments of the present inventive concept.

FIG. 6B is a diagram illustrating a dispersion variation of thespectrometer of FIG. 6A.

FIG. 7A is a block diagram illustrating a spectrometer including adistortion element in addition to a dispersive assembly in accordancewith some embodiments of the present inventive concept.

FIG. 7B is a diagram illustrating a dispersion variation of thespectrometer of FIG. 7A.

FIG. 8A is a block diagram illustrating a spectrometer including adistortion element in addition to a dispersive assembly in accordancewith some embodiments of the present inventive concept.

FIG. 8B is a diagram illustrating a dispersion variation of thespectrometer of FIG. 8A.

FIG. 9A is a block diagram illustrating a spectrometer including adistortion element in addition to a dispersive assembly in accordancewith some embodiments of the present inventive concept.

FIG. 9B is a diagram illustrating a dispersion variation of thespectrometer of FIG. 9A.

FIG. 10 is a block diagram illustrating a spectrometer including adispersive assembly and a distortion element in accordance with someembodiments of the present inventive concept.

FIG. 11 is a block diagram illustrating a spectrometer including adispersive assembly and a distortion element in accordance with someembodiments of the present inventive concept.

FIG. 12A is a block diagram of a spectrometer including a dispersiveassembly in accordance with some embodiments of the present inventiveconcept.

FIGS. 12B-12E are block diagrams illustrating various dispersionassemblies in accordance with some embodiments of the present inventiveconcept.

FIG. 13 is a table illustrating various specifications for the variousdispersive assembly embodiments in accordance with various embodimentsof the present inventive concept.

FIGS. 14A and 14B are graphs illustrating linearization error for both acommon imager and a modified imager including an asphere in accordancewith some embodiments of the present inventive concept.

FIG. 15 is a detailed flow chart illustrating operations ofspectrometers in accordance with some embodiments of the presentinventive concept.

DETAILED DESCRIPTION

The inventive concept will now be described more fully hereinafter withreference to the accompanying drawings, in which embodiments of theinventive concept are shown. This inventive concept may, however, beembodied in many different forms and should not be construed as limitedto the embodiments set forth herein; rather, these embodiments areprovided so that this disclosure will be thorough and complete, and willfully convey the scope of the inventive concept to those skilled in theart.

It will be understood that, when an element is referred to as being“connected” to another element, it can be directly connected to theother element or intervening elements may be present. In contrast, whenan element is referred to as being “directly connected” to anotherelement, there are no intervening elements present. Like numbers referto like elements throughout.

Spatially relative terms, such as “above”, “below”, “upper”, “lower” andthe like, may be used herein for ease of description to describe oneelement or feature's relationship to another element(s) or feature(s) asillustrated in the figures. It will be understood that the spatiallyrelative terms are intended to encompass different orientations of thedevice in use or operation in addition to the orientation depicted inthe figures. For example, if the device in the figures is turned over,elements described as “below” other elements or features would then beoriented “above” the other elements or features. Thus, the exemplaryterm “below” can encompass both an orientation of above and below. Thedevice may be otherwise oriented (rotated 90 degrees or at otherorientations) and the spatially relative descriptors used hereininterpreted accordingly. Well-known functions or constructions may notbe described in detail for brevity and/or clarity.

It will be understood that, although the terms first, second, etc. maybe used herein to describe various elements, these elements should notbe limited by these terms. These terms are only used to distinguish oneelement from another. For example, a first element could be termed asecond element, and, similarly, a second element could be termed a firstelement, without departing from the scope of the present inventiveconcept. As used herein, the term “and/or” includes any and allcombinations of one or more of the associated listed items.

Unless otherwise defined, all terms (including technical and scientificterms) used herein have the same meaning as commonly understood by oneof ordinary skill in the art to which this inventive concept belongs. Itwill be further understood that terms, such as those defined in commonlyused dictionaries, should be interpreted as having a meaning that isconsistent with their meaning in the context of this specification andthe relevant art and will not be interpreted in an idealized or overlyformal sense expressly so defined herein.

Embodiments of the inventive concept are described herein with referenceto schematic illustrations of idealized embodiments of the inventiveconcept. As such, variations from the shapes and relative sizes of theillustrations as a result, for example, of manufacturing techniquesand/or tolerances, are to be expected. Thus, embodiments of theinventive concept should not be construed as limited to the particularshapes and relative sizes of regions illustrated herein but are toinclude deviations in shapes and/or relative sizes that result, forexample, from different operational constraints and/or frommanufacturing constraints. Thus, the elements illustrated in the figuresare schematic in nature and their shapes are not intended to illustratethe actual shape of a region of a device and are not intended to limitthe scope of the inventive concept.

As discussed in the background, U.S. Patent Application Publication No.2009/0040521 entitled EVEN FREQUENCY SPACING SPECTROMETER AND OPTICALCOHERENCE TOMOGRAPHY DEVICE to Hu et al. addresses this relatively highchange in dispersion by a prism air-spaced with respect to a grating.This is also discussed in FOURIER DOMAIN OPTICAL COHERENCE TOMOGRAPHYWITH A LINEAR-IN-WAVENUMBER SPECTROMETER by Hu et al. Hu discusses usingfirst and second dispersive elements, for example, a grating and aprism, separated by an air gap to approximately linearize the dispersionangle as a function of wavenumber, such that uniform spatial sampling atthe detector array equates to sampling at constant frequency, orwavenumber, intervals. However, the use of a grating-air space-prismconfiguration typically requires control of extra degrees of freedom,and adds to the number of glass-air interfaces, potentially reducing theease of manufacture and increasing costs.

As originally discussed in CONSTANT-DISPERSION GRISM SPECTROMETER FORCHANNELED SPECTRA by Traub, a prism-grating (GRISM) structure inintimate contact may be adequate to the task of creating, in thelanguage of Traub, a constant dispersion (k-linear) spectrograph. Traub,however, does not provide a prescription for practical design of a GRISMspectrometer that meets the requirements of FDOCT imaging, including therelationship between required dispersion and degree of linearizationrequired.

Furthermore, Traub's prescription relies on material dispersion of theprism as the primary mechanism of balancing dispersion of the grating.It is however more generally known by Snell's Law that the refractionfrom the exit face of a prism is a nonlinear function of the angle ofincidence to the exit face of the prism and, therefore, that a spectrumwith a first angular dispersion impinging onto a face of a prism willtransit the prism face with a second angular dispersion, not linearlyrelated to the first. This effect dominates material dispersion for lowdispersion glasses. As discussed in, for example, U.S. Pat. No.6,661,513 to Granger, refractive-diffractive spectrometers use thiseffect to position a prism after a dispersive grating, but in intimatecontact, to achieve a wavelength-linearized dispersion function.

As discussed in U.S. Patent Application Publication No. 2008/0088928 toTedesco entitled OPTICAL CONFIGURATIONS FOR ACHIEVING UNIFORM CHANNELSPACING IN WDM TELECOMMUNICATIONS APPLICATIONS, this configuration issufficiently flexible to achieve a wavenumber-linearized dispersionfunction and, as such, a function that is more appropriate to systemsthat rely on frequency-channelized systems than is awavelength-linearized dispersion function. Hu, as noted, extends thisconcept to using refraction at two separate faces of a prism, providingan additional degree of freedom for tuning the output dispersionfunction, but the concept is the same.

Accordingly, some embodiments of the present inventive concept usesequential dispersive functions to both add to total dispersion and totailor the angular dispersion function. For example, in some embodimentsa wavenumber-linearized output function may be achieved using twogratings such that the variation in frequency spacing as imaged alongthe linear detection array will be no greater than about 10%. In someembodiments, a wavenumber-linearized output may be achieved by followinga high dispersion grating with a low dispersion grating, with therelative powers and the angles tuned to the desired function as will bediscussed further herein with respect to FIGS. 3 through 15.

One prescription for a two-grating approach to a wavenumber-linearizedspectrometer for a bandwidth of from about 830 nm to about 930 nmwavelength is given: the prescription presumes a collimated input ofbroadband illumination originating in a single-mode optical fiberdirected to the input face of a first diffraction grating having aspatial frequency of about 1417 lines per mm. The first-order diffractedbeam of the center wavenumber makes an angle alpha_1 relative to theinput beam, and is directed at a second diffraction grating angled suchthat the output angle alpha_2 relative to the original input beam isreduced. In effect, the sign of the diffracted order is inverted afterthe second grating. The effect is that the total first order dispersivepower is approximately the sum of the dispersive powers from the twogratings, but the sign of the derivative of the dispersion with respectto wavelength is flipped, allowing the second grating to compensate forthe variation in dispersion induced by the first grating. Appropriateselection of the two gratings enables the system to be designed fortargeted total dispersion and for approximately constant dispersion withrespect to, for example, wavenumber.

Referring now to FIG. 3A, embodiments of the present inventive conceptincluding a dual grating dispersion assembly will be discussed. Asillustrated in FIG. 3A, the spectrometer 310 includes a light entranceelement 312 (Detector arm fiber) for receiving light from an externalsource. More generally the light entrance element 312 may be referred toas an electromagnetic radiation entrance. The light is passed through afirst set of collimating optics 214 (collimating lens) to a dispersiveassembly 330 including first and second gratings 320 and 322 inaccordance with some embodiments discussed herein. The first and secondgratings 320 and 322 separate the light into various spectra. Theseparated light passes through a second set of focusing optics 318 to adetection element 320 (detector). As used herein, the “focusing optics”318 will be assumed to be an ideal lens set. As is understood by thosehaving skill in the art, many different lens sets can be used for thefocusing optics 318 of the Spectrometer 310 without departing from thescope of the present inventive concept.

Details of some exemplary embodiments illustrated in FIG. 3A will bediscussed. The spectral bandwidth is 100 nm, 1295 cm⁻¹ (inversecentimeters) centered at 880 nm. The first grating 320 with 1417lines/mm at a 45 degree angle of incidence is followed by the secondgrating 322 of 484 lines/mm at a 29 degree angle of incidence. The anglebetween grating 1 and grating 2 is 61.4 degrees. The first grating 320is at angle of 45 degrees with respect to the input beam. The outputfrom the second grating is imaged onto a linear array. As illustrated inFIG. 3B, the spatial increment with respect to wavenumber increment isconstant to within 8.0%, exhibiting a characteristic quadraticdistortion. In other words, using a dual-grating dispersive assembly 330as illustrated in FIG. 3A may lower the variation in dispersion to about8.0%.

Referring now to FIG. 4A, embodiments of the present inventive conceptusing a GRISM as the dispersive assembly will be discussed, such thatthe variation in frequency spacing as imaged along the linear detectionarray will be no greater than about 5%. It will be understood that likereference numerals refer to like elements throughout. Therefore detailswith respect to these elements may not be repeated herein in theinterest of brevity. In embodiments illustrated in FIG. 4A, a 1504line/mm grating is followed by a fused silica prism in intimate contact(GRISM), such that the angular dependence of refraction at the outputface provides the dispersion correction. The apex angle of the prism is60 degrees, and the input beam intersects the grating face at an angleof 44.1 degrees. The spectral dispersion as a function of wavenumbervaries now by 3.3% and still exhibits the characteristic quadraticdistortion. Thus, as illustrated in FIG. 4B, using a GRISM dispersiveassembly 430 as illustrated in FIG. 4A may lower the variation indispersion to about 5.0%. Such a GRISM configuration may be useful forspectrometers with bandwidths ranging from about 1000 cm⁻¹ to about 3000cm⁻¹.

As illustrated in FIG. 5A, the rays 550 image further from the opticalaxis than is desirable. The quadratic distortion is substantiallyequivalent in function to an extension in magnification along thedispersive plane, with pincushion-like distortion behavior. Asillustrated in FIG. 5B, the addition of compensating barrel distortionin the spectrometer imaging lens can offset this pincushion distortion.

Referring now to FIG. 6A, a spectrometer including a dispersive assemblyand a distortion element in accordance with some embodiments of thepresent inventive concept will be discussed. In particular, a distortionelement, for example, wavefront modifier 640, is included to introducebarrel distortion, which compensates for the pincushion distortiondiscussed above with respect to FIGS. 5A and 5B, such that the variationin frequency spacing as imaged along the linear detection array will beno greater than about 1%. The dispersive assembly 630 illustrated inFIG. 6A is similar to the dispersive assembly discussed in the Hu patentdiscussed above. The addition of the distortion element in the system ofFIG. 6A may reduce the resultant dispersion nonlinearity to about 0.4%,an order of magnitude improvement over the uncompensated result asillustrated in FIG. 6B. Thus, the high dispersion, 100 nm, 1295 cm⁻¹system illustrated in FIG. 6A provides a variation in dispersion ofsubstantially less than the 5.0% discussed above.

As illustrated in FIG. 6A, the distortion element (wavefront modifier640) is positioned between the imaging lens 618 and the array detector620. However, it will be understood that embodiments of the presentinventive concept are not limited to this configuration. Embodimentswill be discussed below including an asphere positioned after anuncompensated lens assembly and before the detector array. It will beunderstood that the distortion element can be accomplished using methodsother than a wavefront modifier and can be designed into the opticaltrain, or added to the optical train as an ancillary element withoutdeparting from the scope of the present inventive concept.

Referring now to FIG. 7A, a system with twice the total dispersion (halfthe total bandwidth): 53 nm, 648 cm⁻¹ than the system discussed abovewith respect to FIG. 6A will be discussed. In embodiments illustrated inFIG. 7A, the dispersive assembly 730′ is provided by two strongdispersive stages. The first stage is a 1504 line/mm grating with a 43.4degree angle of incidence, followed by a second stage GRISM including a1504 line/mm grating at 46.8 degree angle of incidence on a 60 degreefused silica prism. The output from the first grating impinges upon thesecond stage grism, increasing the total dispersion to the target level.Exiting from the output face of the second prism, the dispersivefunction is linearized with respect to wavenumber to within 0.5% (FIG.7B) using similar imaging optics 718, including pincushion distortioncompensation 740, as discussed with respect to the 100 nm embodiments ofFIG. 6A.

Referring now to FIG. 8A, a 22 nm bandwidth (259 cm⁻¹), where once againthe dispersion variation is constrained to below 0.6% (FIG. 8B) will bediscussed. As illustrated in FIG. 8A, the dispersive assembly 830″includes two strong dispersive stages. The first stage is a GRISMcomprising a 2189 line/mm grating with a 67.2 degree angle of incidenceon an 85.5 degree fused silica prism, followed by an equivalent secondstage GRISM at 60 degree angle of incidence using similar imaging optics818, including pincushion distortion compensation (840), as discussedabove with respect to the 100 nm embodiments of FIG. 6A.

Referring now to FIG. 9A, a system with 270 nm bandwidth (5020 cm⁻¹)will be discussed. In embodiments illustrated in FIG. 7A, the dispersiveassembly 930′ is provided by two dispersive stages. The first stage is a1504 line/mm grating with a 34.6 degree angle of incidence, followed bya second stage prism with apex angle equal to 31.5 degrees and angle ofincidence of −21.4 degrees. The prism material of the current embodimentis optical glass with refractive index 1.717 and Abbe dispersion value29.5. The prism is followed by a third stage incorporating a secondgrating. The second grating is a 956 line/mm grating at −19.0 degreeangle of incidence.

The output from the first stage grating impinges upon the second stageprism which, in combination with the third stage second gratingdecreases the total dispersion to the target level and corrects thevariation of dispersion with wavenumber. Exiting from the output face ofthe second grating, the dispersive function is linearized with respectto wavenumber to within 0.5% (FIG. 9B) using similar or equivalentimaging optics 918, including pincushion distortion compensation 940, asdiscussed with respect to the 100 nm embodiments of FIG. 6A.

As illustrated in the table of FIG. 12, a system with 180 nm bandwidth(2590 cm¹) can also be realized. In particular, a dispersive assemblyincluding a GRISM including a 770 line/mm grating with a 50.5 degreeangle of incidence on a 32.6 degree fused silica prism may be used. Thissystem may use similar imaging optics and pincushion distortioncompensation as discussed above with respect to the 100 nm embodimentsof FIG. 6A. With the broad bandwidth in these embodiments, thewavenumber linearization error may be about 2.0%.

Addition of an asphere lens as a wavefront modifier is demonstrated toimprove wavenumber linearization error from about 2.2% to about 0.7 asillustrated in FIGS. 14A and 14B. In particular, linearization error fora common imaging lens (i.e. without a wavefront modifier) is about 2.2%,but with the addition of the asphere lens, the linearization error isreduced to about 0.7%. The asphere lens has a first surface radius ofcurvature R1=67.75 mm, a second surface radius of curvature R2=82.5 mm,a thickness of 8.0 mm, and a fourth order asphere coefficient of−1.06e-6 mm⁻³. The asphere lens is added to the system between thecommon lens assembly and the detector array, and in this embodiment isplaced 22 mm in front of the detector array. Thus, the addition of theasphere lens may not require any modification of the lens assembly orspacing adjustments between the lens assembly and detector array. Inother words, there are no additional changes to the optical system butfor the addition of the asphere lens. Accordingly, in some embodimentsthe addition of the asphere lens is a drop-in improvement. One skilledin the art will recognize that while the use of a single asphere tocompensation quadratic pincushion distortion offers certain designbenefits, this distortion may be alternatively compensated in amulti-element lens set comprising spherical lens elements.

The versatility of embodiments of the present inventive concept may leadto a novel and flexible spectrometer design with a number of keyattributes. For example, spectrometers in accordance with embodimentsdiscussed herein may provide a) an ability to transform an inputdispersive function to a target output function; b) a target outputfunction that is linear in wavenumber to better than about 1.0%; c) anoptical imaging system that operates independently of the dispersiverange as long as certain input conditions are met; d) re-use of highcost dispersive components and e) accommodate bandwidth ranges fromabout 250 cm⁻¹ to about 5100 cm⁻¹.

Referring now to FIG. 10, a block diagram of a spectrometer assembly1011 in accordance with some embodiments of the present inventiveconcept will be discussed. As illustrated in FIG. 10, the spectrometerassembly 1011 includes a broadband collimator assay 1013, a dispersiveassembly 1030, and an imaging/detection assembly 1070. The broadbandinput 1012 is provided to a broadband collimator 1014, part of thebroadband collimator assay 1013. The broadband input 1012 from, forexample, a single mode fiber, is collimated 1014 and the collimatedinput 1015 is provided to the dispersive assembly 1030. The dispersiveassembly 1030 acts to create a virtual object at infinity with a givenangular extent and an effective entrance pupil at a given distance fromthe spectrometer imaging lens 1018. The spectrometer imaging lens 1018,any wavefront modifier 1040 (distortion element) and the detector array1020 are included in the image/detection assembly 1070. The imaging lens1018 and wavefront modification 1040 make up the imaging lens system1045. The dispersive assembly 1030 maps the input optical frequencyspectrum to an angular spectrum as a function of wavenumber, and theimaging lens system 1045 further maps this angular spectrum to thedetector array 1020.

The interface between the dispersive assembly 1030 and the spectrometerimaging assembly 1050 is defined by several constraints. The angularrange of the dispersive assembly output is matched to the acceptanceangle of the downstream imaging system. A second constraint is thatoutput beams of the dispersive assembly pass through an effective exitpupil at a location that coincides with and is smaller than the entrancepupil of the subsequent imaging system. Additionally, to achieve a finaldetected spectrum that is linear in wavenumber, the angular rate ofdispersion of the dispersive assembly must be symmetric about thecentral wavenumber of the source spectrum with a second-order variationthat is matched to the compensating distortion in the imaging system.The latter criterion also includes embodiments for which the dispersiveassembly 1030 has negligible second-order variation in the angulardispersion for which an imaging lens assembly without significantdistortion may be employed.

When these conditions are met, the imaging system in accordance withvarious embodiments discussed herein may be paired and interfaced to aplurality of spectral sources and dispersive assemblies. This makes fora flexible spectrometer architecture, some of which are set out in theTable of FIG. 13, with maximum re-use of imaging elements across a broadrange of dispersive power. This flexibility lends itself to a robustvariable-dispersion spectrometer. In particular, in some embodiments, aseries of discrete dispersive assemblies may be formulated such thatthey share a common angular range for different spectral ranges, and maybe assembled on a movable stage. Each of these dispersive assemblies maybe positioned in the spectrometer assembly before the common imagingoptical assembly, such that the angular extent matches the entrancepupil location and field extent of the optical system. Since the inputto the dispersive assembly is a single collimated beam, a sequence offold mirrors may be deployed to align the input beam to the inputorientation of any one of the various interchangeable dispersiveassemblies, examples of which will be discussed below.

As each unique dispersive assembly is positioned within one commonspectrometer assembly, a key attribute of the spectrometer is modifiedwithin one system architecture sharing other critical and costlycomponents and, therefore, provides a series of discrete unique systemswithin one platform. Notable in Spectral Domain Optical CoherenceTomography (SDPCT), this structure enables dynamic switching among theattributes that define the trade-off between axial resolution andimaging depth: imaged bandwidth and frequency sampling interval.

As illustrated in FIG. 11, the spectrometer architecture includes thevarious elements discussed with respect to FIG. 10, in particular, thecommon broadband assay 1112 including the broadband collimator 114; amoveable or variable dispersive assembly 1130; and a commonimaging/detection assembly 1155 including the imaging lens 1118,wavefront modification 1140 (distortion correction) and the detectorarray 1120. As discussed above, the dispersive assembly 1130 may beconfigured to be interchangeable, i.e., the dispersive assembly and betaken out and replace with one of a number of other dispersiveassemblies to create a new spectrometer architecture, thus providing theflexibility discussed above. The dispersive assemblies may include anyof the dispersive assemblies discussed above or any similar assemblywith unique attributes meeting the described constraints withoutdeparting from the scope of the present inventive concept.

It will be understood that although embodiments of the present inventiveconcept are discussed with respect to interchangeable dispersiveassemblies, embodiments of the present inventive concept are not limitedto this configuration. For example, any one or more of the spectrometerarchitectures discussed above ma_(y) be manufactured as a standalonespectrometer without interchangeable parts without departing from thescope of the present inventive concept.

Referring now to FIGS. 12A-E, the dispersive assembly 1230 illustratedin FIG. 12A may be replaced by any of the dispersive assemblies 1230′,1230″, 1230″′ and 1230″″ illustrated in FIGS. 12B-12E respectively. Thusany of the set of wavenumber-linearized dispersive assemblies (12B-12E)covering an order of magnitude in wavenumber range may be dropped into acommon optical platform, i.e. the spectrometer illustrated in FIG. 12.Like reference numerals refer to like elements through and, thus, thedetails of the spectrometer will not be repeated herein. According tosome embodiments of the inventive concept illustrated in FIGS. 12A-12E,a spectrometer system for four distinct dispersive assemblies coveringfrom 2590 cm⁻¹ (inverse centimeters) to 259 cm⁻¹ may be provided. Thedetails of each of these exemplary systems are detailed in the Table ofFIG. 13.

For a spectrometer having a fixed detector array, i.e. defined by anumber of detection elements and spacing therebetween, the finest axialresolution is limited by the total spectral bandwidth, and the maximumimaging depth is constrained by the finest frequency sampling interval;high resolution mandates wide bandwidth, with limited depth, and deepimaging requires fine sampling interval over a narrow bandwidth, andtherefore poor axial resolution.

For Optical Coherence Tomography applications using a 4096 elementdetector array, such as a Basler Sprint CMOS array that is commerciallyavailable, embodiments discussed herein may provide one master systemwith variable depth ranging (as measured in air) from about 4.0 mm toabout 40 mm, respectively, and with minimum axial resolutions from about17 μm to about 1.7 μm, respectively. This may enable a single system forocular applications ranging, for example, from ultra-high resolution ofthe retina to whole eye biometry (axial length measurements), providingexceptional economy of scale for ocular research, clinical examinations,and intrasurgical imaging. Such a system would allow very uniqueapplications. For example, in ophthalmology, whole eye imaging with anorder of magnitude dynamic range in depth and resolution attributeswould allow single platform integration of high speed optical biometry(measurement of eye length and distances between all eye structuresalong the optical axis) using the 22 nm dispersive assembly, full 3Dimaging of the entire anterior segment from cornea apex to posteriorlens capsule in the setting with the 53 nm dispersive assembly, zoomingin to the anterior chamber or lens capsule alone at the 100 nm setting,and observing tissue fine structure in the cornea or retina at thebroadest bandwidth setting. In each case, optical resolution isoptimized for the depth range of interest, and all measurements areaccomplished with the same optical engine. This zoom function has neverpreviously been demonstrated for spectral domain OCT.

In accordance with some embodiments, the zoom capability offers uniqueopportunity to perform whole eye analytics at multiple scales with asingle console. One such work flow is outlined in the flowchart of FIG.13. As illustrated therein, first, the axial properties of the whole eyeare imaged using the narrowest bandwidth dispersive system,appropriately filtered source (to avoid excess radiation outside of thedetected band), and a deep depth of field (DOF) telecentric optic. Thisfirst image set provides eye length as well as a signature thatindicates distances to all key features in the eye, albeit with limitedresolution of, for example, 20 μm. This distance map then providesdistance values for feeding into the instrument settings to imagespecific regions of the eye as desired.

Stepping up in bandwidth, the next region might be to image the fullanterior segment from cornea apex to behind the lens capsule, coveringall of the refractive elements of the eye in one view, with a 16 mmrange at better than 10 um resolution. Switching to retinal imagingoptics, this 16 mm view would provide a broader range of the posteriorchamber than has been heretofore possible, and may be vital to certaintypes of vitreoretinal surgery.

The next step in bandwidth enables an 8 mm view at better than 5 micronresolution for anterior chamber imaging from cornea to iris, or imagingof the entire lens capsule at high resolution. The 8 mm view may also bean appropriate window for vitreoretinal surgery.

And finally, ultrahigh resolution imaging of any specific targetedstructures from retina to cornea, with bandwidths from 100 nm to 300 nm,and correspondingly restricted depths, is enabled.

It will be understood that the configurations discussed herein are notlimited to the wavelength range or bandwidths, to wavenumber linearizedsystems, to application in OCT, or to applications in ophthalmology. Forexample, embodiments discussed herein may be used in Raman or nearinfrared (NIR) spectroscopy, for example, where a broadband bandwidthhas utility in uncovering a broad fingerprint response, and a narrowerbandwidth enables examination of spectroscopic fine structure. Othersskilled in their respective art will find other applications and otherdetailed implementations that are served by the concepts of thisinventive concept.

In the drawings and specification, there have been disclosed exemplaryembodiments of the inventive concept. However, many variations andmodifications can be made to these embodiments without substantiallydeparting from the principles of the present inventive concept.Accordingly, although specific terms are used, they are used in ageneric and descriptive sense only and not for purposes of limitation,the scope of the inventive concept being defined by the followingclaims.

That which is claimed is:
 1. A variable bandwidth wavenumber-linearizedarray spectrometer, the spectrometer comprising: an input configured toreceive broadband electromagnetic radiation from an external source;collimating optics configured to collimate the received broadbandelectromagnetic radiation; a first dispersive assembly comprising atleast two diffractive elements, wherein a received collimatedelectromagnetic radiation wavefront is dispersed into an outputwavenumber-dependent angular spectrum by an action of the at least twodiffractive elements, the wavenumber-dependent angular spectrum definedby a first wavenumber range and an angular range; a lens assembly thatfocuses the spectrally dispersed radiation such that the wavenumberincrement is substantially constant with respect to spatialincrement-along a line of focus in a plane of dispersion; a detectorarray positioned with respect to the line of focus to receive thedispersed electromagnetic radiation; and a second dispersive assemblycomprising at least two diffractive elements, wherein a receivedcollimated electromagnetic radiation wavefront is dispersed into anoutput wavenumber-dependent angular spectrum by an action of the atleast two diffractive elements, the wavenumber-dependent angularspectrum defined by a second wavenumber range and a second angularrange, the second wavenumber range being a subset of the firstwavenumber range, and the second angular range being substantiallyequivalent to the first angular range; wherein the spectrometer isconfigurable for at least two modes of operation, wherein when operatingin a first mode of operation the first dispersive assembly is positionedalong an optical path between the collimating optics and the detectorarray; wherein when operating in a second mode of operation the seconddispersive assembly is positioned along the optical path between thecollimating optics and the detector array; and wherein the firstdispersive assembly differs from the second dispersive assembly by atleast one physical attribute other than rotation of one or more opticalelements about an axis of rotation of the one or more optical elements.2. The spectrometer of claim 1, wherein the dispersive assemblycomprises a prism.
 3. The spectrometer of claim 1, wherein the first andsecond dispersive assemblies are configured to be interchangeable. 4.The spectrometer of claim 1, wherein a first wavenumber range is nogreater than about 5100 cm⁻¹ and a second wavenumber range is no greaterthan about 250 cm⁻¹.
 5. The spectrometer of claim 1, wherein the firstand second dispersive assemblies are different dispersive assembliessuch that only one of the first dispersive assembly and the seconddispersive assembly is positioned in the spectrometer at a single pointin time.